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Altitude Dependent Thrust Schedules
标准号：
AIR5924
标准名称： Guidelines for the Integration of Electronic Engine Control Systems with Transport Category Aircraft Systems
同源图形
Station Definitions
Typical FADEC System
Example of Thrust vs
Normal Mode Thrust S
Logic for Mode Selec
Engine Idle Selectio
Example of Multiplie
Thrust Schedule Usin
Thrust Rating Select
Ambient Temperature
Thrust* as a Functio
Moving Thrust Lever
Non-Moving Thrust Le
All Engines Operatin
One Engine Inoperati
Typical Cross-Manifo
Typical Body or Nace
Total Air Temperatur
Non-Aspirated TAT Pr
Engine Inlet Mounted
Typical FADEC Select
Typical Presentation
Typical FADEC Engine
Typical EICAS System
相关图形
FIGURE 1 - (See 5.11
AIR1075A
BAROMETRY
FIGURE 11 - GROUND T
AIR1678B
Uncertaint
GENERAL FLIGHT TEST
AIR1678B
Uncertaint
EXAMPLE PRELIMINARY
AIR1678B
Uncertaint
IN-FLIGHT THRUST MEA
AIR1678B
Uncertaint
CORRECTED THRUST VER
AIR1678B
Uncertaint
X-31A Thrust Vector
AIR4253A
Descriptio
FIGURE 3 - AIT Altit
AIR5320
Summary of
PROPULSIVE EFFICIENC
AIR5450
Advanced D
EFFECT OF PRESSURE L
AIR5450
Advanced D